Hi everyone,I need a code for designing a diverging section of a 2-D and 3-D supersonic nozzle and being able to plot it with different numbers of points using methods of charecteristics, please email and let me know if there is a way to get this.
Thanks.
I know that sivells approach is good, who has his code? His program published in his article"A Computer Program for the Aerodynamic Design of Axisymmetric and Planar Nozzles for Supersonic and Hypersonic Wind Tunnels". Who has written this program? Please send me, thank you.yazixiu@126.com